Solid-propellant gas generator assemblies and methods
AssigneeGoodrich Corporation
InventorsBrian Wilson, Kevin Mueller
Life of this patent
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Abstract
A solid-propellant gas generator assembly may comprise a bulkhead having an orifice disposed in a housing. The bulkhead may be disposed between a first end and a second end of the housing. The bulkhead and the first end may define a propellant cavity. The bulkhead and the second end may define a pressure chamber. A fast burning solid-propellant may be disposed in the propellant cavity. The solid-propellant gas generator assembly may be configured to replace a slow burning solid-propellant gas generator system in a solid-propellent gas generator system.
Claims5
A method of retro-fitting a solid-propellant gas generator system, the method comprising:
- removing a first cartridge assembly from the solid-propellant gas generator system, the first cartridge assembly including a first solid-propellant;
- and
- coupling a second cartridge assembly to the solid-propellant gas generator system, the second cartridge assembly including a second solid-propellant configured to burn faster than the first solid-propellant, wherein:
- the first cartridge assembly includes a first housing defining a first cavity extending from a first end of the first housing to a second end of the first housing,
- the first solid-propellant is disposed in the first cavity of the first housing,
- a first flow of gas from burning the first solid-propellant is configured to flow unobstructed in the first cavity;
- the second cartridge assembly further comprises a bulkhead having an orifice disposed in a second housing of the second cartridge assembly,
- the second cartridge assembly further comprises a propellant cavity defined between a first end of the second housing and the bulkhead and a pressure chamber defined between the bulkhead and a second end of the second housing,
- the orifice of the second cartridge assembly is configured to meter a flow of gas into the pressure chamber of the second cartridge assembly, and
- a pressure in the propellant cavity of the second cartridge assembly and the pressure chamber of the second cartridge assembly equalize over time in response to burning the second solid-propellant.
Dependencies are inferred from the claim text.